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It is design suitable for engineering in the field of missiles Aerodynamics and attempts to present a rational and unified account of the principal results of missiles aerodynamics. It si divided into 10 chapters. Chapter 1- is purely introductory of the Character, Chapter 2-Collects Together for Convenient use many of the Result used repeatedly in subsequent Chapters, Chapter 3- treat the subject of slender-body theory has the great advantage that it is mathematically tractable in a very wide range of missiles Configurations, Chapter 4 to 8 - an attempt is made to present missiles aerodynamics in an orderly building up of missile from its Component parts, the body alone, the wing panels, the tail and the control Surfaces. Chapter 6 - discussed the aerodynamics of a tail behind the wings of the missiles depends on the flow field of the wing-body combination, Chapter 7 - treat the important subjects of drag Stability derivatives. The nature of aerodynamics drag makes desirable a separate Chapter devoted to drag. The Chapter on Stability derivatives attempts to treat all forces and Moment on a missile (other then drag) from a general and unified point of view.
- Introduction
- Some formula Commonly used in missiles aerodynamics
- Slender-body at supersonic and subsonic speed
- Aerodynamic of Bodies; Vortices
- Wing-body interference
- Downwash, sidewash, and the wake
- Wing-tail Interference
- Aerodynamics Controls
- Drag
- Stability Derivatives
http://rapidshare.de/files/22493320/Nielsen_J.N._-_Missile_Aerodynamics__McGraw_Hill_1960_.pdf
